OrbitalInfo/src/OrbitalInfo.cpp

#include <OrbitalInfo.h>

OrbitalInfo::OrbitalInfo(){
  absTime = 0;
  OBT = 0;
  pkt_num = 0;

  lon = 0.;
  lat = 0.;
  alt = 0.;

  Bnorth = 0.;
  Beast = 0.;
  Bdown = 0.;
  Babs = 0.;
  BB0 = 0.;
  L = 0.;

  londip = -1000.;
  latdip = -1000.;
  altdip = -1000.;

  loncgm = -1000.;
  latcgm = -1000.;
  altcgm = -1000.;

  loncbm = -1000.;
  latcbm = -1000.;
  altcbm = -1000.;

  std::fill_n(cutoff, 20, 0.);

  // Quaternions
  q0 = -1000.;
  q1 = -1000.;
  q2 = -1000.;
  q3 = -1000.;

  // Euler angles (nadir reference frame)
  theta = -1000.;
  phi = -1000.;
  etha = -1000.;

  // Euler angles (local field reference frame)
  thetamag = -1000.;
  phimag = -1000.;
  ethamag = -1000.;

  std::fill_n(goodAttitude, 5, 0);
}


void OrbitalInfo::Clear(){
  absTime = 0;
  OBT = 0;
  pkt_num = 0;

  lon = -1000.;
  lat = -1000.;
  alt = -1000.;

  Bnorth = -1000.;
  Beast = -1000.;
  Bdown = -1000.;
  Babs = -1000.;
  BB0 = -1000.;
  L = -1000.;

  londip = -1000.;
  latdip = -1000.;
  altdip = -1000.;

  loncgm = -1000.;
  latcgm = -1000.;
  altcgm = -1000.;

  loncbm = -1000.;
  latcbm = -1000.;
  altcbm = -1000.;

  std::fill_n(cutoff, 20, 0.);

  // Quaternions
  q0 = -1000.;
  q1 = -1000.;
  q2 = -1000.;
  q3 = -1000.;

  // Euler angles (nadir reference frame)
  theta = -1000.;
  phi = -1000.;
  etha = -1000.;

  // Euler angles (local field reference frame)
  thetamag = -1000.;
  phimag = -1000.;
  ethamag = -1000.;

  std::fill_n(goodAttitude, 5, 0);
}

/**
 * Fills a struct cOrbitalInfo with values from a OrbitalInfo object (to put data into a F77 common).
 */
void OrbitalInfo::GetLevel2Struct(cOrbitalInfo *l2) const{
  l2->abstime  = absTime;
  l2->obt      = OBT;
  l2->pkt_num  = pkt_num;

  l2->lon = lon;
  l2->lat = lat;
  l2->alt = alt;

  l2->Bnorth = Bnorth;
  l2->Beast = Beast;
  l2->Bdown = Bdown;
  l2->Babs = Babs;
  l2->BB0 = BB0;
  l2->L = L;

  l2->londip = londip;
  l2->latdip = latdip;
  l2->altdip = altdip;

  l2->loncgm = loncgm;
  l2->latcgm = latcgm;
  l2->altcgm = altcgm;

  l2->loncbm = loncbm;
  l2->latcbm = latcbm;
  l2->altcbm = altcbm;

  memcpy(l2->cutoff, cutoff, sizeof(cutoff));

  // Quaternions
  l2->q0 = q0;
  l2->q1 = q1;
  l2->q2 = q2;
  l2->q3 = q3;

  // Euler angles (nadir reference frame)
  l2->theta = theta;
  l2->phi = phi;
  l2->etha = etha;

  // Euler angles (local field reference frame)
  l2->thetamag = thetamag;
  l2->phimag = phimag;
  l2->ethamag = ethamag;

  memcpy(l2->goodAttitude, goodAttitude, sizeof(goodAttitude));
}

void OrbitalInfo::SetFromLevel2Struct(cOrbitalInfo *l2){
  absTime  = l2->abstime;
  OBT      = l2->obt;
  pkt_num  = l2->pkt_num;

  lon = l2->lon;
  lat = l2->lat;
  alt = l2->alt;

  l2->Bnorth = Bnorth;
  l2->Beast = Beast;
  l2->Bdown = Bdown;
  l2->Babs = Babs;
  BB0 = l2->BB0;
  L = l2->L;

  londip = l2->londip;
  latdip = l2->latdip;
  altdip = l2->altdip;

  loncgm = l2->loncgm;
  latcgm = l2->latcgm;
  altcgm = l2->altcgm;

  loncbm = l2->loncbm;
  latcbm = l2->latcbm;
  altcbm = l2->altcbm;

  memcpy(cutoff, l2->cutoff, sizeof(l2->cutoff));

  // Quaternions
  q0 = l2->q0;
  q1 = l2->q1;
  q2 = l2->q2;
  q3 = l2->q3;

  // Euler angles (nadir reference frame)
  theta = l2->theta;
  phi = l2->phi;
  etha = l2->etha;

  // Euler angles (local field reference frame)
  thetamag = l2->thetamag;
  phimag = l2->phimag;
  ethamag = l2->ethamag;

  memcpy(goodAttitude, l2->goodAttitude, sizeof(l2->goodAttitude));
}

ClassImp(OrbitalInfo)
1	#include <OrbitalInfo.h>
2
3	OrbitalInfo::OrbitalInfo(){
4	absTime = 0;
5	OBT = 0;
6	pkt_num = 0;
7
8	lon = 0.;
9	lat = 0.;
10	alt = 0.;
11
12	Bnorth = 0.;
13	Beast = 0.;
14	Bdown = 0.;
15	Babs = 0.;
16	BB0 = 0.;
17	L = 0.;
18
19	londip = -1000.;
20	latdip = -1000.;
21	altdip = -1000.;
22
23	loncgm = -1000.;
24	latcgm = -1000.;
25	altcgm = -1000.;
26
27	loncbm = -1000.;
28	latcbm = -1000.;
29	altcbm = -1000.;
30
31	std::fill_n(cutoff, 20, 0.);
32
33	// Quaternions
34	q0 = -1000.;
35	q1 = -1000.;
36	q2 = -1000.;
37	q3 = -1000.;
38
39	// Euler angles (nadir reference frame)
40	theta = -1000.;
41	phi = -1000.;
42	etha = -1000.;
43
44	// Euler angles (local field reference frame)
45	thetamag = -1000.;
46	phimag = -1000.;
47	ethamag = -1000.;
48
49	std::fill_n(goodAttitude, 5, 0);
50	}
51
52
53	void OrbitalInfo::Clear(){
54	absTime = 0;
55	OBT = 0;
56	pkt_num = 0;
57
58	lon = -1000.;
59	lat = -1000.;
60	alt = -1000.;
61
62	Bnorth = -1000.;
63	Beast = -1000.;
64	Bdown = -1000.;
65	Babs = -1000.;
66	BB0 = -1000.;
67	L = -1000.;
68
69	londip = -1000.;
70	latdip = -1000.;
71	altdip = -1000.;
72
73	loncgm = -1000.;
74	latcgm = -1000.;
75	altcgm = -1000.;
76
77	loncbm = -1000.;
78	latcbm = -1000.;
79	altcbm = -1000.;
80
81	std::fill_n(cutoff, 20, 0.);
82
83	// Quaternions
84	q0 = -1000.;
85	q1 = -1000.;
86	q2 = -1000.;
87	q3 = -1000.;
88
89	// Euler angles (nadir reference frame)
90	theta = -1000.;
91	phi = -1000.;
92	etha = -1000.;
93
94	// Euler angles (local field reference frame)
95	thetamag = -1000.;
96	phimag = -1000.;
97	ethamag = -1000.;
98
99	std::fill_n(goodAttitude, 5, 0);
100	}
101
102	/**
103	* Fills a struct cOrbitalInfo with values from a OrbitalInfo object (to put data into a F77 common).
104	*/
105	void OrbitalInfo::GetLevel2Struct(cOrbitalInfo *l2) const{
106	l2->abstime = absTime;
107	l2->obt = OBT;
108	l2->pkt_num = pkt_num;
109
110	l2->lon = lon;
111	l2->lat = lat;
112	l2->alt = alt;
113
114	l2->Bnorth = Bnorth;
115	l2->Beast = Beast;
116	l2->Bdown = Bdown;
117	l2->Babs = Babs;
118	l2->BB0 = BB0;
119	l2->L = L;
120
121	l2->londip = londip;
122	l2->latdip = latdip;
123	l2->altdip = altdip;
124
125	l2->loncgm = loncgm;
126	l2->latcgm = latcgm;
127	l2->altcgm = altcgm;
128
129	l2->loncbm = loncbm;
130	l2->latcbm = latcbm;
131	l2->altcbm = altcbm;
132
133	memcpy(l2->cutoff, cutoff, sizeof(cutoff));
134
135	// Quaternions
136	l2->q0 = q0;
137	l2->q1 = q1;
138	l2->q2 = q2;
139	l2->q3 = q3;
140
141	// Euler angles (nadir reference frame)
142	l2->theta = theta;
143	l2->phi = phi;
144	l2->etha = etha;
145
146	// Euler angles (local field reference frame)
147	l2->thetamag = thetamag;
148	l2->phimag = phimag;
149	l2->ethamag = ethamag;
150
151	memcpy(l2->goodAttitude, goodAttitude, sizeof(goodAttitude));
152	}
153
154	void OrbitalInfo::SetFromLevel2Struct(cOrbitalInfo *l2){
155	absTime = l2->abstime;
156	OBT = l2->obt;
157	pkt_num = l2->pkt_num;
158
159	lon = l2->lon;
160	lat = l2->lat;
161	alt = l2->alt;
162
163	l2->Bnorth = Bnorth;
164	l2->Beast = Beast;
165	l2->Bdown = Bdown;
166	l2->Babs = Babs;
167	BB0 = l2->BB0;
168	L = l2->L;
169
170	londip = l2->londip;
171	latdip = l2->latdip;
172	altdip = l2->altdip;
173
174	loncgm = l2->loncgm;
175	latcgm = l2->latcgm;
176	altcgm = l2->altcgm;
177
178	loncbm = l2->loncbm;
179	latcbm = l2->latcbm;
180	altcbm = l2->altcbm;
181
182	memcpy(cutoff, l2->cutoff, sizeof(l2->cutoff));
183
184	// Quaternions
185	q0 = l2->q0;
186	q1 = l2->q1;
187	q2 = l2->q2;
188	q3 = l2->q3;
189
190	// Euler angles (nadir reference frame)
191	theta = l2->theta;
192	phi = l2->phi;
193	etha = l2->etha;
194
195	// Euler angles (local field reference frame)
196	thetamag = l2->thetamag;
197	phimag = l2->phimag;
198	ethamag = l2->ethamag;
199
200	memcpy(goodAttitude, l2->goodAttitude, sizeof(l2->goodAttitude));
201	}
202
203	ClassImp(OrbitalInfo)